Flat Wing Area
72.4644 m²
Entry Into service
1983-10-01
Maximum Take-Off Weight
23.8136 t (paragliders: kg)
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All data (25 fields)
- Name
- Lockheed F-117 Nighthawk
- Manufacturer
- Lockheed Corporation
- Description
- The Lockheed F-117 Nighthawk is a retired American single-seat, subsonic, twin-engined stealth attack aircraft developed by Lockheed's Skunk Works division and operated by the United States Air Force (USAF).
- ICAO Code
- F117
- First Flight
- 1981-06-18
- Entry Into service
- 1983-10-01
- Production End
- 1990-01-01
- Designer
- Lockheed Corporation
- Length (m)
- 19.812
- Height (m)
- 3.6576
- Cockpit Crew
- 1
- Max Speed (km/h)
- 1100.087
- Max Ceiling (m)
- 13716
- Armament
- 2 × internal weapons bays with one hardpoint each (total of two weapons) equipped to carry:; Bombs:; GBU-10 Paveway II laser-guided bomb with 2,000 lb Mk84 blast/fragmentation or BLU-109 or BLU-116 Penetrator warhead; GBU-12 Paveway II laser-guided bomb with 500 lb Mk82 blast/fragmentation warhead; GBU-27 Paveway III laser-guided bomb with 2,000 lb Mk84 blast-fragmentation or BLU-109 or BLU-116 P…
- Max Mach (Mach)
- 0.92
- National Origin
- United States of America
- Number Built
- 64
- Powerplant Description
- 2 × General Electric F404-F1D2 turbofan engines
- Primary Users
- United States Air Force
- Status
- Retired from combat in 2008, used as training aircraft as of 2025
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/Lockheed_F-117_Nighthawk
- Flat Wing Span (m)
- 13.1064
- Flat Wing Area (m²)
- 72.4644
- Wake Category
- M
- Number of Engines
- 2